CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle
This paper presents the Computational Fluid Dynamic (CFD) analysis to study the effect geometry and flow parameters on thrust force created by the flow from convergent divergent nozzles to a suddenly expanded circular duct of larger cross-sectional area. The study is focusing on resultant thrust f...
| Main Authors: | , , |
|---|---|
| Format: | Proceeding Paper |
| Language: | English |
| Published: |
IEEE
2017
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/60790/ http://irep.iium.edu.my/60790/1/08226302.pdf |
| _version_ | 1848785550927986688 |
|---|---|
| author | Pathan, Khizer Ahmed Khan, Sher Afghan Dabeer, P. S. |
| author_facet | Pathan, Khizer Ahmed Khan, Sher Afghan Dabeer, P. S. |
| author_sort | Pathan, Khizer Ahmed |
| building | IIUM Repository |
| collection | Online Access |
| description | This paper presents the Computational Fluid Dynamic (CFD) analysis to study the effect geometry and flow parameters on thrust force created by the flow from convergent divergent
nozzles to a suddenly expanded circular duct of larger
cross-sectional area. The study is focusing on resultant thrust force. The nozzles are designed for Mach numbers 1.1, 1.4, 1.8 and 2.0. The CFD analysis is done by varying the area ratios and nozzle pressure ratios for all Mach numbers. The area ratios considered for the analysis are 1, 2, 4, 6, 8, 10 and 12. The values of nozzle pressure ratios considered in the analysis are 2, 4, 6, 8, 10 and 12. The results for different combinations of Mach number, area ratios and nozzle pressure ratios are compared with the help of tables. By observing all the results it can be concluded that the resultant thrust force created by flow through
nozzle is strongly influenced by Mach number, area ratio and
Nozzle pressure ratio. |
| first_indexed | 2025-11-14T16:54:56Z |
| format | Proceeding Paper |
| id | iium-60790 |
| institution | International Islamic University Malaysia |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-14T16:54:56Z |
| publishDate | 2017 |
| publisher | IEEE |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | iium-607902017-12-26T10:59:50Z http://irep.iium.edu.my/60790/ CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle Pathan, Khizer Ahmed Khan, Sher Afghan Dabeer, P. S. T Technology (General) T175 Industrial research. Research and development TL Motor vehicles. Aeronautics. Astronautics This paper presents the Computational Fluid Dynamic (CFD) analysis to study the effect geometry and flow parameters on thrust force created by the flow from convergent divergent nozzles to a suddenly expanded circular duct of larger cross-sectional area. The study is focusing on resultant thrust force. The nozzles are designed for Mach numbers 1.1, 1.4, 1.8 and 2.0. The CFD analysis is done by varying the area ratios and nozzle pressure ratios for all Mach numbers. The area ratios considered for the analysis are 1, 2, 4, 6, 8, 10 and 12. The values of nozzle pressure ratios considered in the analysis are 2, 4, 6, 8, 10 and 12. The results for different combinations of Mach number, area ratios and nozzle pressure ratios are compared with the help of tables. By observing all the results it can be concluded that the resultant thrust force created by flow through nozzle is strongly influenced by Mach number, area ratio and Nozzle pressure ratio. IEEE 2017-12-21 Proceeding Paper PeerReviewed application/pdf en http://irep.iium.edu.my/60790/1/08226302.pdf Pathan, Khizer Ahmed and Khan, Sher Afghan and Dabeer, P. S. (2017) CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle. In: 2017 2nd International Conference for Convergence in Technology (I2CT), 7-9 April 2017, Pune, Maharashtra, India. http://ieeexplore.ieee.org/document/8226302/ 10.1109/I2CT.2017.8226302 |
| spellingShingle | T Technology (General) T175 Industrial research. Research and development TL Motor vehicles. Aeronautics. Astronautics Pathan, Khizer Ahmed Khan, Sher Afghan Dabeer, P. S. CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle |
| title | CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle |
| title_full | CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle |
| title_fullStr | CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle |
| title_full_unstemmed | CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle |
| title_short | CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle |
| title_sort | cfd analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle |
| topic | T Technology (General) T175 Industrial research. Research and development TL Motor vehicles. Aeronautics. Astronautics |
| url | http://irep.iium.edu.my/60790/ http://irep.iium.edu.my/60790/ http://irep.iium.edu.my/60790/ http://irep.iium.edu.my/60790/1/08226302.pdf |